Motion simulator

ABSTRACT

A MOTION SIMULATOR CAPABLE OF MOTION IN ALL SIX DEGRESS OF FREEDOM IS PROVIDED HAVING A PLATFORM PROVIDING THREE POINTS IN A PLANE AND A SUPPORT BASE PROVIDING THREE POINTS IN ANOTHER PLANE. SIX EXTENSIBLE MEMBERS ARE EMPLOYED EACH CONNECTED AT ONE END TO THE SUPPORT BASE AND AT THE OTHER END TO THE PLATFORM AND CONNECTING ADJACENT POINTS OF THE SUPPORT BASE AND PLATFORM, THE EXTENSIBLE MEMBERS BEING POWERED AND CONTROLLED FOR PROVIDING ANY OF THE MOTIONS OF THE PLATFORM BY SELECTIVE CHANGES IN LENGTH OF THE EXTENSIBLE MEMBERS. MEANS ON THE PLATFORM IS PROVIDED FOR EXPERIENCING MOTION PRODUCED BY MOVEMENT OF THE PLATFORM.

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Feb. 9, 1971 Re. 27,051

MOTION SIMULATOR Original Filed Dec. '7, 1964 6 Sheets-Sheet a FIGJO.

. mvznTon; KLAUS L.CAPPEL ATTYS.

United States Patent Int. Cl. G09b 9/08 US. Cl. 3512 Claims Matterenclosed in heavy brackets appears in the original patent but forms nopart of this reissue specification; matter printed in italics indicatesthe additions made by reissue.

ABSTRACT OF THE DISCLOSURE A motion simulator capable of motion in allsix degrees of freedom is provided having a platform providing threepoints in a plane and a support base providing three points in anotherplane. Six extensible members are employed each connected at one end tothe support base and at the other end to the platform and connectingadjacent points of the support base and platform, the extensible membersbeing powered and controlled for providing any of the motions of theplatform by selective ehan'ges in length of the extensible members.Means on the platform is provided for experiencing motion produced bymovement of the platform.

The present invention relates to a motion simulator and, moreparticularly, to an improved motion simulator for producing fore, andaft, lateral, elevational, roll, pitch and yaw movements, or anycombination of such movements.

The present invention is concerned primarily with dynamic simulators inwhich the component parts are connccted and actuated by rigid elements,such as linear actuators or the like. In such systems, dynamicsimulators are classified according to the extent to which motion of thecomponents producing displacement in any of the six degrees of freedomis achieved. The six degrees of freedom comprise three mutuallyperpendicular axes of linear movement and three axes of rotationalmovement, one of the axes being normal to the other two. The dynamicsimulator of the present invention belongs to that class oflinear-actuated dynamic simulators which employs a coupled system forproducing movement of the platform, that is, movement is achieved bycoupled forces produced by the linear actuators as opposed to acombination of superimposed pure translational or rotational movementwith the possibility that movements may occur requiring only one of theactuators, with all other actuators unaffected.

In the prior art of linear-actuated coupled-motioned dynamic simulatorsin an advanced preferred embodiment, a platform or table is supported bythree vertically-extending linear actuators with threehorizontallypositioned linear actuators, all of which are extensible forsimulation of movement of the platform. The vertical groups of actuatorsin addition to supporting the platform primarily produce vertical lineartranslation and pitch and roll motions of the platform, and thehorizontal group of actuators are typically positioned at adjacentcorners of the platform for stabilizing the platform and producinglinear movement in two directions and yaw movement. As a result of thisarrangement of the horizontal linear actuators, the support base area ofthe motion simulator has been very large and the vertical columns whichsupport the horizontal actua- Re. 27,051 Reissued Feb. 9, 1971 tors haveby necessity been very large, requiring a mas sive foundation to providethe rigidity to insure accurate response to command signals extendingthe actuators and to provide a reference frame for the platform which isimmovable. The cost of the foundation of these prior art simulators hascomprised a considerable portion of the total cost of the simulator.Moreover, because of the massiveness of the foundation, the simulatorhas not been movable to different locations.

The linear-actuated coupled-motion dynamic motion simulator of thepresent invention is far more flexible in its use than simulators of theprior art. In accordance with the present invention, the platformprovides three points in one plane and the support base provides threepoints in another plane such that the points on the base and theplatform define the vertices of triangular faces of an octahedron. Theplatform is supported above the base by six powered and controlledlinear actuators connecting each of the three points on the support basewith two adjacent points on the platform, whereby the linear actuatorsand lines in the platform and support base, respectively, drawn betweenthe points of connection, all define the edges of the triangular facesof the octahedron. This truss arrangement of connecting the linearactuators between the platform and support base without sacrifice offreedom of movement provides a greater compactness and rigidity of thesystem than heretofore provided in prior art motion simulators. Greateconomy also results from the simulators much smaller foundationsupporting the actuators with no massive lateral support columnsrequired for necessary rigidity. The much smaller foundation required bythe present invention permits a structure which is not only lessexpenive to build but also so light in weight that it may be made easilyportable, i.e., capable of having the structure as fabricated moved todifferent locations. The great compactness of the simulator results alsoin a saving of space at the location where the simulator is used.

For a better understanding of these and other features and advantages ofthe present invention, reference is made to the following detaileddescription and the accompanying drawings, in which:

FIG. 1 is a perspective view of a typical prior art motion simulator;

FIG. 2 is a plan view of the motion simulator of the present invention;

FIG. 3 is a side elevational view of the motion simulator of the presentinvention showing the platform providing a gimbal mount for a capsulerotatable about its support axes and showing the capsule in full linesin its upright position and dashed lines when rotated about the supportaxes;

FIG. 4 shows a front elevational view of the embodiment of the inventionof FIG. 3;

FIG. 5 is a sectional view taken along line 5-5 of FIG. 4;

FIG. 6 is a schematic side elevational view similar to FIG. 3 of thepresent invention;

FIG. 7 is a schematic front elevational view similar to FIG. 4;

FIG. 8 is a schematic representation of the present inventionillustrating one possible extension of the linear actuators forsimulated movement of the platform;

FIG. 9 is a front elevational view of the platform position and linearactuators shown in FIG. 8;

FIG. 10 is a schematic view of the present invention illustratinganother possible extension of the linear actuators for simulatedmovement of the platform;

FIG. 11 is a front elevational view of the platform position and linearactuators shown in FIG. 10;

FIG. 12 is a schematic side elevational view of the inventionillustrating still another possible extension of the linear actuatorsfor simulated movement of the platform;

FIG. 13 is a front elevational view of the platform position and linearactuators shown in FIG. 12;

FIG. 14 illustrates another embodiment of the platform and capsule;

FIG. 15 is a front elevational view of the embodiment of the platformand capsule shown in FIG. 14;

FIG. 16 is a schematic hydraulic flow diagram of the apparatus foractuating the linear actuators of the present invention;

FIG. 17 is a schematic diagram illustrating one form of a mechanicalanalog for an uncoupled-motion dynamic simulator connected at its innergimbal to an analog of the present invention; and

FIG. 18 is a schematic circuit diagram of the system for converting frommovement of the analog of FIG. 17 to movement of the actuators of thepresent invention.

Referring first to FIG. 1, a typical prior art motion simulator isschematically represented therein. This linear-actuated coupled-motionprior art simulator has a rectangular-shaped platform 10 supported abovea base foundation 12. The platform may be used as shown for helicopterflight simulation and the like, or may support a capsule or the like forsimulation of movement as would be experienced in space flight. Theplatform 10 is generally supported above the rectangular-shapedfoundation 12 by means of three vertical linear actuators 14, 16 and 18positioned beneath the platform, actuators 14 and 16 being positioned atadjacent comers of edge 10a of the platform and actuator 18 beingpositioned intermediate the ends of opposite edge 10b of the platform,for example. Actuators 14, 16 and 18 are primarily responsible forvertical linear movement and pitch and roll movements of the platform.

Other movements of the platform are accomplished primarily by means ofhorizontal linear actuators 20, 2'2 and 24 applying force at variouscorners of the platform along edges thereof, actuator 20 applying forceat the intersection of edges 10b and 10c and parallel to edges 10b,actuator 22 applying force at the intersection of edges 10b and 10d andparallel to edges 10d, and actuator 24 applying force at theintersection of edges 10a and 10b and parallel to edge 10a. Each of thehorizontal actuators 20, 22 and 24 are supported at their outwardlyextending ends by means of large rigid columns 26, 28 and 30,respectively, made of steel reinforced concrete and supported on amassive foundation 12 also made of reinforced concrete. The columns 26,28 and 30 must be very large and massive to preclude any movement, dueto the thrust of the actuators, which might modify the reference frameof the platform. The large columns and platform have involved an expensewhich has been a considerable portion of the cost of the simulator andhave precluded any possibility of portability of the simulator.

In contrast to the prior art, the present invention, as shown in FIGS.2, 3 and 4, may have a support base 32 with only slightly larger surfacearea than platform 33 supported thereabove. Also, each of the six linearextensible actuators 34, 35, 36, 37, 38 and 39 are mounted to extendbetween the support base and the platform. More specifically, thesupport base provides three support points 40, 41 and 42 and theplatform provides three support points 44, 45 and 46. In practice theso-called points are areas and usually two closely spaced areas.However, it will be understood that such areas are preferably placed asclosely together as possible, and points as used herein include areasnot spaced as closely as possible but whose spacing does not precludethe functioning described hereafter. The relative positions of thepoints in the support base and platform, respectively, are such thatthey define vertices of a hexagon when projected on one of the planes,as can be seen in FIG. 2.

The six extensible actuators 34, 35, 36, 37, 38 and 39 are connectedbetween adjacent points on the platform and support base, actuator 34between points 40 and 46, actuator 35 between points and 44, actuator 36between points 44 and 41, actuator 37 between points 41 and 45, actuator38 between points and 42, and actuator 39 between points 42 and 46. Thearrangement of the simulator is such that the actuators lie on the linesbetween points in the platform and support base which define edges of anoctahedron having only triangular faces. Each pair of actuatorsconnected at one of the points on the support base 32 or platform 33 isoffset slightly from being mounted both at the exact same point due tothe inherent limitation of space, size of the actuators and angle atwhich each meets the respective base and platform. It is desirable tohave the actuators of each pair connected at each point offset from oneanother the least amount possible, i.e., attached as closely to the samepoint as possible, in order to minimize the external forces appliedalong the actuators. Otherwise, if the actuators at each point areoffset from one another any substantial amount, bending in theconnections adjacent the platform and base will occur and toggle effectswill be set up. In addition increased spacing between the pair ofactuators will cause deflection in the structure and set up additionalunwanted forces acting on the actuators.

As can be seen in FIGS. 4 and 5, each of the linearextensible actuators34, 35, 36, 37, 38 and 39 is provided with two universal joints, oneadjacent each end at the mounting of the actuator to the base 32 andplatform 33, respectively. Actuator 34 has universal joints 54 and 56;actuator 35 has universal joints 5-8 and 60; actuator 36 has universaljoints 62 and 64; actuator 37 has universal joints 66 and 6S; actuator38 has universal joints 70 and 72; and actuator 39 has universal joints74 and 76. The

shafts supporting the universal joints are aligned axially with therespective actuators to which they are coupled.

FIG. 5 illustrates a sectional view of linear actuator 35, which isrepresentative of all six of the actuators. In accordance with thepresent invention in providing a simple, light-weight and highlyflexible system, the actuator 35 comprises an inner cylindrical tubularsleeve and a coaxial outer cylindrical tubular sleeve 82, sleeve 80being secured to the flat circular end 82a of outer tube 82. Slidablysupported between the inner sleeve and outer sleeve is a coaxialtelescopic cylindrical tubular piston member 84 which may be extendedand retracted to provide the effective linear extension and contractionof the actuator. The telescopic cylindrical piston member 84 has apiston head portion 84a at the bottom thereof with a wall thickness ofslightly smaller dimension than the spacing between the outer diameterof inner sleeve 80 and the inner diameter of outer sleeve 82, and thewall thickness of the rest of the tubular piston member comprisingpiston sleeve 84b is reduced from that of the piston head. The pistonmember is slightly longer than the inner and outer sleeves, and fitsover the outer diameter of the inner sleeve. Fixedly located along theouter diameter of the lesser wall thickness sleeve 84b of piston member84 and along the lower portion of the piston member is a bearing stopring 85, having a wall thickness slightly less than the distance betweenthe outer diameter of the piston sleeve 84b and the inner diameter ofouter sleeve 82. A second bearing stop ring 86 is provided adjacent thebottom of piston head 84a in a groove along outer diameter of the pistonhead provided therefor. The bearing stop rings 85 and 86 limit theupward and downward movement of the piston sleeve 84b, respectively, byabutment against stops 88 and 89, respectively. Stops 88 and 89 areprovided by inwardly projecting flanges around the inner diameter of.outer sleeve 82 adjacent the top and bottom thereof. The distancebetween the bearing stop rings 85 and 86 associated with the pistonmember is sufficient to provide stability and rigidity of the actuatorwhen the piston member is telescoped to maximum extension. The bearingstop rings 85 and 86 serve to resist lateral forces between the piston84 and outer sleeve 82 and the stop rings provide guidance of the pistonmember.

The upper end of inner sleeve 80 has annular cap 92 firmly seatedthereon by, in the present instance, screwing a threaded tubular flangeof the cap inside an internally threaded portion of inner sleeve 80. Theupper end of outer sleeve 82 is also provided with an annular cap 94,having an annular internally threaded flange portion screw over athreaded portion along the outside of outer sleeve 82. The outerdiameter of annular cap 92 and the inner diameter of annular cap 94snugly accommodate sleeve 84b in a sliding fit. Also located at theupper end of outer sleeve 82 along the inner diameter thereof is abearing ring 98 press fitted therein and abutting against the upper sideof stop 88. The piston member 84 slides between bearing ring 98 and theinner sleeve for support at the upper end of the inner and outersleeves.

As previously explained, each actuator is provided with a universaljoint at each end thereof through which they are coupled to the base 32and platform 33. As can be seen in FIG. 5, which is a typical showing ofthe actuators, the universal joints 58 and 60 associated with actuatorare coupled to the actuator at lower end 82a of outer sleeve 82 and atthe upper end of piston sleeve 84b, respectively.

The extension and retraction of the linear actuators is accomplished bymeans of a hydraulic system to be explained hereafter. Thefluid'pressure is supplied to the actuators through hoses, one adjacenteach end of the outer sleeve. More particularly, as shown in FIG. 5, ahose 102 is secured to a hose connection fitting adjacent the bottom ofouter sleeve 82 so that fluid enters the cylinder formed by sleeves 80and 82 slightly below the abutment surface of stop 89. A second hose 104is connected by a suitable fitting adjacent the top of outer sleeve 82so that fluid enters sleeve 82 slightly above the abut ment surface ofstop 88. When the piston member is to be telescoped, fluid is fedthrough hose 102 into the lower chamber 106 between the inner and outersleeves, thereby exerting pressure against the bottom of piston head 84aforcing the piston member upward. The distance the piston member istelescoped depends on the amount of fluid introduced which may be afunction of time. In the preferred manner of operating the actuatorsduring extension of the piston member, as the fluid flows into the lowerchamber 106, fluid flows out of the upper chamber 108 through hose 104and through the hydraulic system for filling the lower chamber. In orderto prevent fluid passage around the piston head 84a resulting in loss ofmotive force, 0 rings 110, 112, 114 and v116 are staggered incircumferential grooves alternately opening inwardly and outwardly alongthe inner and outer diameters of the piston head. The 0 rings whichbottom in the groove also extend beyond the surface in which the grooveis formed and against the outer face of inner tubular sleeve 80 andagainst the inner face of outer tubular sleeve 82, respectively. As analternate arrangement, 0 rings 110 and 114 could be eliminated and aclearance allowed between inner sleeve 80 and piston member 84.

In order to avoid leakage of fluid at the point of exit from thecylinder of piston slee've 84b, the outer edge of cap 92 and the inneredge of cap 94 are provided with outwardly and inwardly openingcircumferential grooves, respectively, containing 0 rings 118 and 120which extend into contact with and seal against the opposite sides ofthe piston member. When it is desired to retract the extended pistonmember 84, fluid flows through hose 104 into the top of the upperchamber 108 and out of the bottom of the lower chamber 106 through hose102. The top portion of bearing stop ring 85, in addition to providing astop limiting the extension of actuator 35, as well as the shoulderflange opposite the face on piston head 84a, provides a piston face forthe fluid flowing into the actuator through hose 104. The smallerworking area is compensated for by the efl'ect of gravity on theplatform acting to tend to retract the actuator. Thus, the fluidentering the actuator through hose 104 pushes the piston face of bearingstop ring and the back flange of piston head 84a downward, retractingthe piston member into the actuator as fluid flows out of the lowerchamber 106 through hose 102. In this manner by reversing the flow offluids in hoses 102 and 104, the actuators are extended and retracted toproduce movement of the platform.

The piston member in the actuator is arranged to resist bucklingunder,load by making it tubular rather than a rod of the same crosssectional area. Nevertheless, the piston area is not the full diameterof the tube and in fact is much less than this by making the cylinderand hence the piston head annular. By keeping the spacing between theinner and outer sleeves small, the fluid volume required to move theactuator is much reduced. For illustration, the relative sizes of thestructure in each actuator for one arrangement of the simulator maycomprise an unextended actuator of 8 feet length having an extension of5 feet with the inner diameter of the outer sleeve being 6% inches, theouter diameter of the inner sleeve being 6 inches and the outer diameterof the lesser wall thickness portion of the piston member being 6%inches. In this arrangement the platform may weigh approximately 2,500pounds, and the actuator may have a maximum piston velocity of 60inches/ second produced by a horsepower hydraulic power supply operatingall the pistons. FIG. 16 illustrates one hydraulic system for anactuator of the present invention. The system shown is illustrative ofthe hydraulic system for each of the actuators, each actuator having aseparate hydraulic system corresponding thereto. In FIG. 16 there isschematically shown a hydraulic actuator cylinder with two supply lines122 and 124 connected thereto on opposite sides of piston 126 forsupplying fluid to move the piston 126 in the actuator cylinder 120. Thefluid is pumped into the hydraulic system from hydraulic pump 128 whichmoves the fluid through restriction 130 to provide the desired maximumvelocity of the fluid flowing through the system. The fluid fromrestriction 130 passes through solenoid controlled shut-off valve 132which is opened when energized to allow flow therethrough, but in caseof power failure will be actuated closed for disconnecting automaticallythe supply line. The fluid passing through valve 132 is coupled by fluidpressure suply line 133 to the pressure input connection of a four-wayservo valve 134. The valve selec tively channels the flow of fluid tothe cylinder at one side or the other of piston 126 through supply line122 or 124. The opposite side of the cylinder is connected to the drainor sump line 135 through servo valve 134. A solenoid controlledtwo-position shut-off valve 136 is connected in drain line 135 betweenthe output port of the servo valve 134 and the sump 140. Solenoidshut-off valve 136 is maintained in an open position when energizedproviding a through path to sump 140, which serves as a reservoir forthe fluid in the hydraulic system from which pump 128 is supplied. Inorder to maintain proper pressure of the fluid flowing into the system,there is provided a sup ply line 142 from the pressurized sump 140, thesupply line being divided to connect to supply lines 122 and 124 throughcheck valves 144 and 146, respectively, which allow flow from thepressurized sump in the event the pressure drops below a predeterminedminimum level upon failure of the system while the actuator is inmotion. There is also incorporated into the system two relief valves 148and 150 connected to supply lines 122 and 124, respectively, so as toprotect the cylinder 120 in case of failure of the servo valve 134. Incase of power failure all of the actuators will be locked and the supplylines would be depressurized automatically. The pressure in the systemmay be on the order of 2,000 pounds per square inch.

With this medium pressure, relatively low volume system, standardpetroleum-base fluid may be used as the actuating fluid.

In operation of the system of FIG. 16, when it is desired to extendpiston 126 in cylinder 120, a command signal is given to actuate servovalve 134 to connect fluid pressure supply line 133 with supply line 124and drain line 135 with supply line 122. Consequently, the main supplyline will supply fluid through supply line 124 to raise piston andsupply line 122 connected to drain line 135 allows the fluid in theupper chamber of the cylinder to be discharged to the sump. When thedesired extension is reached, the servo is cut off disconnecting themain supply line.

When it is desired to retract piston .126 in cylinder 120, the servovalve 134 is moved to connect the fluid pressure supply line 133 withsupply line 122 and drain line 135 with supply line 124. By thisconnection, the fluid pumped through the fluid pressure supply line ischanneled through supply line 122 to the cylinder above the piston,thereby driving the piston downwardly, the fluid from the lower chamberbeing forced out through supply line 124 and drain line 135 to sump 140.After the piston reaches the desired position, the solenoid valve isdeenergized and returned to neutral position.

Whenever the servo valve 134 is in neutral position the equal pressurethat is supplied to both sides of the piston from the pressurized sumpsupply assures that the piston maintains its selected position withinthe cylinder.

Platform 33 which is manipulated to simulate move ments, such as wouldbe encountered in helicopter maneuvers or in space flight, may have awide variety of forms. As shown in FIGS. 2, 3 and 4, platform 33 has agenerally irregular hexagonal-shaped outer periphery with a largeopening through the center forming an inner hexagonalshaped periphery.The platform provides a gimbal mount within housings 152 for shaft 154.Shaft 154 supports capsule 156 and provides an axis of rotation for agross pitch motion of the capsule. Capsule 156 may be of any of the typecommonly in use in testing durability and physical and mental reactionsof astronauts under space flight conditions. The capsule may have anyshape which would fit within the inner periphery of the hollow platform33 and be capable of generally 90 of rotation about its gimbal mount, asshown in FIGS. 2 and 3, without striking the platform. The capsule wouldordinarily be provided with a crew compartment (not shown). The capsulemay be driven about shaft 154 by any convenient means such as a motor orhydraulic chain drive or the like (not shown). In this manner,additional pitch of the capsule is provided over that achieved bymovement of linear actuators supporting the platform.

As previously stated, the platform may have a wide variety of forms andmay support a number of different types of compartments. Particularlyimportant is a compartment for simulating helicopter flight conditions.As shown in FIGS. 14 and 15, the platform 160 supported by the actuatorshas a semi-elliptical shape supporting a compartment 162 having a flatrectangular-shaped front extending back to be inwardly and downwardlycurved to the periphery of the platform, as is typical in helicoptercockpits. Such a capsule and platform arrangement as described in regardto FIGS. 14 and 15 may be used with simulators producing movementsencountered in helicopier flight.

As previously described, the linear actuators may be :xtended in variouscombinations to simulate movement at the platform to various positionswith respect to the vase, thereby simulating fore and aft, lateral,elevational, 'oll, pitch or yaw movements, or any combination of thesenovements. Since the present invention employs a highly :oupled systemwith the linear actuators, all actuators may )e displaced upon movementof any of them even if the aarticular actuator is one which is notextended or retracted to produce the desired movement. FIGS. 6am] 7 areschematic illustrations of the motion simulator of the present inventionshowing a side elevational view and a front elevational view,respectively, similar to views in FIGS. 3 and 4. In FIGS. 8 and 9 thereis shown a side elevational view and a front elevational view,respectively, of the motion simulator in which actuators 37 and 38 havebeen extended equal distances to produce movement which simulatesprimarily a pitch motion. FIGS. 10 and 11 illustrate side elevationaland front elevational views, respectively, of the simulator withactuators 35 and 36 extended to produce a combination of rotationalmovements of the platform. Still another position of movement of theplatform is shown in the side elevational and front elevational views inFIGS. 12 and 13, respectively, where all of the actuators have beenextended different lengths to produce a complex movement of the platformwhich is a combination of the movements capable of being produced by thesimulator.

In order to determine accurately the movements of the actuators forproducing any of the three linear movements or any of the threerotational movements associated with the three mutually perpendicularaxes of a reference frame, coordinate conversion between the couplesystem, such as employed in the present invention, and the referenceframe is necessary. The coordinate conversion is accomplished reliably,simply and inexpensively by use of a mechanical analog conversionsystem. In the mechanical analog the geometric arrangement of a set ofsix transducers fixed at one end to a reference plane and at the otherend to a movable platform is exactly similar but reduced in scale to thearrangement of the six actuators of the motion simulator. As the analogplatform is manipulated, its supports corresponding to the actuatorsextend and retract in a manner directly analogous to the manner in whichthe actuators extend and retract in the actual simulator in assuming thedesired positions. As shown in FIG. 17, the outputs of a mechanicalanalog 163 are in terms of signals representative of the extensions orretractions of the supports of the model corresponding to the actuatorsdriven by that signal in the actual platform. The amount that each ofthe six linear actuators should be extended or retracted in order toproduce the desired movement of the platform in accordance with movementin the uncoupled system is thus produced by the combination of signals.The mechanical analog to be explained fully hereafter is of an uncoupledmotion system. Any one or any combination of the six degrees ofindividual movement, roll, pitch, yaw, vertical, fore and aft, andlateral, are the inputs to the mechanical analog. Each of the sixoutputs of the mechanical analog corresponds to the actuation requiredfor an associated actuator in the coupled motion system of the presentinvention.

In FIG. 17 one complete actuator system connected to the mechanicalanalog is shown for simplicity, the actuator system for actuator 39; theother five actuator systems are similar in arrangement. The output ofthe mechanical analog associated with actuator 39 is connected to adifferential amplifier 164, which provides an amplified signal foractuation of the servo valve 165 in the proper direction for extensionor retraction of actuator 39, as

previously described in regard to the servo valveand hydraulic system ofFIG. 16.

A potentiometer 166 is mechanically coupled to the piston member in theactuator for providing an error signal feedback loop 168 to thedifferential amplifier 164 indicating the present position of the pistonmember with respect to a fixed reference level in the actuator. Thedifference signal between that feedback from the potentiometer and theoutput from the mechanical analog is amplified through the differentialamplifier for controlling the servo valve to have the piston memberextended or retracted the remaining desired distance.

A tachometer generator 170 is also mechanically coupled to the pistonmember of the actuator along the same mechanical coupling as thepotentiometer for providing an output signal indicative of the speed atwhich the piston member is being moved. The latter output signal issupplied to compensating circuits 172. The compensating circuits have anon-linear transfer characteristic such that a higher gain is providedfor large input signals than for small input signals. The output of thecompensating circuits is connected through feedback loop 174 to thedifferential amplifier 164. The differential amplifier provides anoutput signal which is the difference signal between the signals fromthe mechanical analog and the potentiometer, the difference signal beingsummed with the signal from the compensating circuits. By this circuitarrangement, additional speed of movement of the piston member isprovided during the initial phases of movement thereof, the speed ofmovement being decreased as the desired extension or retraction of thepiston member is approached.

A representation of one possible form of the mechanical analog 163 isillustrated schematically in FIG. 18, which shows an uncoupled motionsystem generally designated 180 mechanically coupled to an analog modelof a coupled motion system 182 of the present invention. The uncoupledmotion system 180 comprises generally a support base 184 which includesan apparatus, such as electric servo motor, for raising and loweringvertical shaft 186. Vertical shaft 1 86 supports a horizontallyextending track 188 on which rides carriage 190 which thereby moves onlyin the direction of the extension of its track. Carriage 190 supportsthereon a horizontally extending track 192 which extends perpendicularto the direction of movement of carriage 190. A carriage 194 on track192 is guided thereby to move only in the direction of the track. Thecarriage 194, in turn, supports a vertically extending shaft 196, whichis rotatable about its vertical axis. Vertically extending shaft 196supports at its upper end a yoke 198, which provides a gimbal mount atopyoke arms 198a and 198b to receive trunnions 200a and 200b,respectively, supporting ring 202 for rotation about the horizontaltrunnion axis. Across a second diameter of ring perpendicular to thetrunnion axis, a trunnion 204 rotatably supports platform simulatingdisc 206. Any of the possible uncoupled linear or rotational movementschange the position of the platform disc 206 which is the heart of theanalog model to which the transducer elements analogous to the actuatorson the actual platform are coupled at one end. The transducer elementsare coupled at their other end to base 208, which is fixed by struts orother suitable supports (not shown) to ground or structure fixed toground like "base 184. The transducers are shown in an arrangementsimilar to the arrangement of the actuators in FIG. 7 and are numberedcorrespondingly to those actuators. Each transducer is electricallyconnected to a system such as described with actuator 39 in FIG. 17. Thesignal from each transducer is indicative of the amount its associatedactuator should be extended or retracted. The transducers may be slidingtap resistance strips connected across a source of power and providing avoltage output at the tap indicative of the position of a movable tapalong the resistance strip.

The uncoupled motion analog of FIG. 18 provides a system wherein linearmovement of selected direction, amount and velocity, may be made alongany one or any combination of the three mutually perpendicular axesprovided by shaft 186, carriage 190 and carriage 194. By proportioningthese movements to the scale of the model relative to the platform, theplatform may therefore be positioned at any selected three dimensionalcoordinate position. The uncoupled rotational movements about the axesof shaft 196, trunnions 200a and 20% and trunnion 204, respectively, maybe individually selected to cause the platform to follow the analog inits rotation about individual or combined axes alone or superimposed onlinear movements. The movement of the elements of the uncoupled motionanalog may be performed manually or by small servo drives associatedwith each of the elements for actuating changes in relative position ofthe elements. In actual use the command signals to the six servo driveswould be received from a computer which in turn receives command inputsfrom various sources, one of which may be an operator on the motionsimulator.

It will be observed that the present invention provides a light platformposition simulator and one which may be transported to desired locationsafter fabricated since there are no rigid lateral columns and largesupporting foundation. Moreover, the platform not only providesflexibility of movement but permits rapid and accurate movement inresponse to command signals coupled from the mechanical analog. Thearrangement of the six linear actuators in an octahedron configurationprovides stability and economy of space.

While the invention has been described with particular reference to aspecific embodiment thereof, it will be understood that it may beembodied in a large variety of forms different from the one specifcallyshown and described without departing from the scope and spirit of theinvention as defined by the appended claims.

I claim:

[1. A motion simulator capable of motion in all six degrees of freedom,three linear and three rotational, or any combination thereof,comprising:

a platform providing three points in a plane;

a support base providing three points in another plane;

and

six powered and controlled extensible members each connected at one endto the support base and at the other end to the platform and connectingadjacent points of the support base and platform f r providing any ofsaid motions by said platform by selective changes in length of saidextensible memhere, said extensible members and lines in the platformand support base, respectively, drawn between points defined edges of anoctahedron having only triangular faces] [2. a motion simulator capableof motion in all six degrees of freedom, three linear and threerotational, or any combination thereof, comprising:

a. platform providing generally three points in a plane;

a support base providing generally three points in another plane suchthat the points on said base and platform define vertices of a hexagonwhen projected vertically on one of said planes; and

six powered and controlled extensible members each connected at one endto the support base and at the other end to the platform and connectingadjacent points of said base and said platform for providing any of saidmotions by said platform by selective changes in length of saidextensible members, said extensible members and lines in said platformand support base, respectively, drawn between points generally definingedges of an octahedron having only triangular faces] [3. A motionsimulator capable of motion in all six degrees of freedom, three linearand three rotational, or any combination thereof, comprising:

a platform defining three points in a plane;

a support base defining three points in another plane;

and

six powered and controlled extensible members connected in pairs at oneend on each of said three points of said base, each member of said pairbeing connected adjacent the other member of that pair; said extensiblemembers connected in pairs to said base having the other ends of eachpair respectively connected at the nearer of two of the three points onsaid platform such that each point on said base and platform have a pairof extensible members connected thereat adjacent each other, saidextensible members providing any of said motions by said 1 1 platform byselective changes in length of said extensible members, said extensiblemembers and lines in said platform and support base drawn between pointsgenerally defining edges of an octahedron having only triangular faces][4. The motion simulator of claim 3 in which said extensible memberseach comprise a telescopic tubular member slidable along a first supportelement located within said tubular member and slidable within a secondsupport element, said tubular member providing a piston face, saidmotion simulator further comprising hydraulic means connectable to eachof said extensible members for exerting force against said piston facesfor extending said extensible members] [5. The motion simulator of claim4 in which each of said tubular members includes another piston face;said first-mentioned piston face and said other piston face beingassociated with respective extension and retraction of said tubularmembers; said hydraulic means being coupled to each of said extensiblemembers at two positions, one above maximum upward movement of saidother piston face and another below maximum downward movement of saidfirst-mentioned piston face.]

6. An acceleration simulator capable of motion in all six degrees offreedom, three linear and three rotational,

or any combination thereof, comprising:

a platform providing three points in a plane;

a support base providing three points in another plane;

means on the platform for experiencing acceleration effects produced bymovement of the platform;

six extensible members, two of the extensible members connected fromeach point of the support base to separate points in the platform forproviding any of the motions by the platform by selective changes inlength of the extensible members; and

a control system for actuating the selective changes in length of theextensible members producing acceleration of said means for determiningefiects on said means or response of any occupant of said means.

7. An acceleration simulator capable of motion in all six degrees offreedom, three linear and three rotational, or any combination thereof,comprising:

a platform providing three points in a plane;

a support base providing three points in another plane;

means on the platform for an occupant experiencing acceleration effectsproduced by movement of the platform;

six extensible members, two of the extensible members connected fromeach point of the support base t separate points in the platform forproviding any of the motions by the platform by selective changes inlength of the extensible members; and

a control system for actuating the selective changes in length of theextensible members for producing acceleration of said means.

8. An acceleration simulator capable of motion in all six degrees offreedom, three linear and three rotational. or arty combination thereof,comprising:

a platform providing three points in a plane;

a support base providing three points in another plane;

means on the platform for experiencing acceleration effects produced bymovement of the platform;

six powered extensible members each connected at one end to the supportbase and at the other end to the platform and connecting adjacent pointsof the support base and platform for providing any of said motions bysaid platform by selective changes in length of said extensible members,said extensible members Cir and lines in said platform and support base,respec- 9. The acceleration simulator of claim 8 in which the extensiblemembers are hydraulically actuatable, and the control system includeshydraulic means connected to each of the extensible members foractuating the selective changes in length of the extensible members.

10. An acceleration simulator capable of motion in all six degrees offreedom, three linear and three rotational, or any combination thereof,comprising:

a platform providing generally three points in a plane;

a support base providing generally three points in another plane suchthat the points on said base and platform define vertices of a hexagonwhen projected vertically on one of said planes;

means on the platform for experiencing acceleration effects produced bymovement of the platform;

six powered extensible members each connected at one end to the supportbase and at the other end to the platform and connecting adjacent pointsof said base and said platform for providing any of said motions by saidplatform by selective changes in length of said extensible members, saidextensible members and lines in said platform and support base,respectively, drawn between points generally defining edges of anoctahedron having only triangular faces; and

a control system for actuating the selective changes in length of theextensible members producing acceleration of said means for determiningeffects on said means or response of any occupant of said means.

11. The acceleration simulator of claim 10 in which the extensiblemembers are hydraulically actuatable, and the control system includeshydraulic means connected to each of the extensible members foractuating the selective changes in length of the extensible members.

12. An acceleration simulator capable of motion in all six degrees offreedom, three linear and three rotational, or any combination thereof,comprising: i

a platform providing three points in a plane;

a support base providing three points in another plane;

means on the platform for an occupant experiencing acceleration effectsproduced by movement of the platform;

six powered extensible members connected in pairs at one end of each ofsaid three points of said base, each member of said pair being connectedadjacent the other member of that pair; said extensible membersconnected in pairs to said base having the other ends of each pairrespectively connected at the nearer of two of the three points on saidplatform such that each point on said base and platform have a pair ofextensible members connected thereat adjacent each other, saidextensible members providing any of said motions by said platform byselective changes in length of said extensible members, said extensiblemembers and lines in said platform and support base drawn between pointsgenerally defining edges of an octahedron having only triangular faces;and

a control system for actuating the selective changes in length of theextensible members for producing acceleration of said means.

13. The acceleration simulator of claim 12 in which the extensiblemembers are hydraulically actuatable, and the control system includeshydraulic means connected to each of the extensible members foractuating the selective changes in length of the extensible members.

14. The acceleration simulator of claim 12 in which said extensiblemembers each comprise av telescopic tubular member slidable along afirst support element located within said tubular member and slidablewithin a second support element, said tubular member providing a pistonface, said acceleration simulator further comprising hydraulic meatnsconnectable to each of said extensible members for exerting forceagainst said piston faces for extending said extensible members.

15. The acceleration simulator of claim 14 in which each of said tubularmembers includes another piston face; said first-mentioned piston faceand said other piston face being associated with respective extensionand retraction of said tubular members; said hydraulic means beingcoupled to each of said extensible members at two positions, one abovemaximum upward movement of said 5 other piston face and another belowmaximum downward movement of said first-mentioned piston face.

References Cited 10 The following references, cited by the Examiner, areof record in the patented file of this patent or the original patent.

UNITED STATES PATENTS 14 3,078,594 2/1963 White 35-12 3,085,354 4/1963Rasmussen et al 3512 OTHER REFERENCES Gough: Contribution to Discussionsto Papers on Research in Automobile Stability and Control and in TypePerformance, by Cornell Staff," Proc. Automobile Division, Institutionof Mechanical Engineers, 1956-57, pp. 392-394.

Gough and Whitehall: Universal Type Test Machine, Free. NinthInternational Technical Congress F.I.S.I.T.A., May 1962, pp. 117-137(Institution of Mechanical Engineers).

German textbook Grundlagen des Systematischen Getriebeaufbaus, by RobertKraus, pp. 155159, published 1952.

JEROME SCHNALL, Primary Examiner P. V. WILLIAMS, Assistant Examiner

